A Force and Moment Test of a 1/24-Scale F-111 Model at Mach Numbers from 0.7 to 1.3.
ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AFS TN
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A test program was conducted in the Propulsion Wind Tunnel 16T to determine forces and moments on a 124-scale F-111 model. Data were obtained at Mach numbers from 0.7 to 1.3 at total pressures of 1200 and 2000 psfa. Model angle of attack was varied from -2 to 20 deg at 0-deg sideslip. Sideslip angles were varied from -10 to 10 deg at 10- and 15-deg angles of attack. Author
- Attack and Fighter Aircraft